GB1076076A - Fabric reinforced plastic product and method of making same - Google Patents
Fabric reinforced plastic product and method of making sameInfo
- Publication number
- GB1076076A GB1076076A GB16658/65A GB1665865A GB1076076A GB 1076076 A GB1076076 A GB 1076076A GB 16658/65 A GB16658/65 A GB 16658/65A GB 1665865 A GB1665865 A GB 1665865A GB 1076076 A GB1076076 A GB 1076076A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sections
- parallel
- fabric
- section
- opposite pair
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 239000004744 fabric Substances 0.000 title abstract 6
- 238000004519 manufacturing process Methods 0.000 title abstract 3
- 239000002990 reinforced plastic Substances 0.000 title abstract 3
- 239000000853 adhesive Substances 0.000 abstract 1
- 230000001070 adhesive effect Effects 0.000 abstract 1
- 239000000463 material Substances 0.000 abstract 1
- 230000003014 reinforcing effect Effects 0.000 abstract 1
Classifications
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
- E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
- E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
- E04C2/36—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels
- E04C2/365—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels by honeycomb structures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
- B29C70/228—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure the structure being stacked in parallel layers with fibres of adjacent layers crossing at substantial angles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/0089—Producing honeycomb structures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B31—MAKING ARTICLES OF PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER; WORKING PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER
- B31D—MAKING ARTICLES OF PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER, NOT PROVIDED FOR IN SUBCLASSES B31B OR B31C
- B31D3/00—Making articles of cellular structure, e.g. insulating board
- B31D3/02—Making articles of cellular structure, e.g. insulating board honeycombed structures, i.e. the cells having an essentially hexagonal section
- B31D3/0223—Making honeycomb cores, e.g. by piling a plurality of web sections or sheets
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
- B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2793/00—Shaping techniques involving a cutting or machining operation
- B29C2793/0081—Shaping techniques involving a cutting or machining operation before shaping
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
- Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
- Y10T156/1003—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by separating laminae between spaced secured areas [e.g., honeycomb expanding]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24149—Honeycomb-like
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Textile Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Laminated Bodies (AREA)
- Panels For Use In Building Construction (AREA)
- Making Paper Articles (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
Abstract
1,076,076. Laminates. HEXCEL PRODUCTS Inc. April 20, 1965 [April 20, 1964], No. 16658/65. Heading B5N. A method of making a fabric reinforced plastic honeycomb structure in which the warp and woof of the reinforcing fabric are disposed at oblique angles relative to the longitudinal axes of cells of the structure comprises providing a plurality of non-rectangular parallelogram shaped cut sections of fabric reinforced plastic material of substantially the same pattern and size, and in which the warp of the fabric extends parallel and the woof of the fabric extends perpendicular to a first opposite pair of parallel sides of each section and at oblique angles in reference to a second opposite pair of parallel sides of each said section; applying adhesive on to one side of each section along spaced apart mutually parallel bonding lines extending substantially perpendicularly to said first opposite pair of parallel sides of the non- rectangular parallelogram sections and superimposing said sections one upon the other in a stack and with the bonding lines of successive said superi mposed sections staggered relative to one another, treating the stack to form permanent bonds between adjacent sections to build up a block of unexpanded honeycomb structure. The block may be out along lines parallel to said second opposite pair of parallel sides of each section and expanded. The cores may be used in the production of sandwich laminates.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US360955A US3321355A (en) | 1964-04-20 | 1964-04-20 | Fabric reinforced plastic product and method of making same |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1076076A true GB1076076A (en) | 1967-07-19 |
Family
ID=23420067
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB16658/65A Expired GB1076076A (en) | 1964-04-20 | 1965-04-20 | Fabric reinforced plastic product and method of making same |
Country Status (4)
Country | Link |
---|---|
US (1) | US3321355A (en) |
JP (1) | JPS5146782B1 (en) |
DE (1) | DE1504368B1 (en) |
GB (1) | GB1076076A (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1500981A (en) * | 1966-08-26 | 1967-11-10 | Three-dimensional structure and its manufacturing processes | |
US3673058A (en) * | 1969-04-07 | 1972-06-27 | Hexcel Corp | Honeycomb having laminates of unidirectional strands |
WO1991004779A1 (en) * | 1989-09-27 | 1991-04-18 | Klaus Rennebeck | Process for the production of a semi-finished article, and uses of the article thus produced |
US5128192A (en) * | 1990-02-02 | 1992-07-07 | Northrop Corporation | Braided preform process for thermoplastic honeycomb cores |
FR2691923B1 (en) * | 1992-06-04 | 1994-09-09 | Europ Propulsion | Honeycomb structure in thermostructural composite material and its manufacturing process. |
CN110185915B (en) * | 2019-05-10 | 2020-11-06 | 国家能源投资集团有限责任公司 | Method and apparatus for producing thermoplastic composite core material |
CN110242848B (en) * | 2019-05-10 | 2020-11-06 | 国家能源投资集团有限责任公司 | Thermoplastic composite core material |
CN110242849B (en) * | 2019-05-10 | 2020-11-06 | 国家能源投资集团有限责任公司 | Thermoplastic composite core and device comprising same |
CN110509616A (en) * | 2019-09-02 | 2019-11-29 | 嘉兴恒诺蜂窝制品有限公司 | A kind of preparation method of aluminium honeycomb core |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2477852A (en) * | 1945-07-04 | 1949-08-02 | Owens Corning Fiberglass Corp | Structural panel construction |
US2594838A (en) * | 1947-03-04 | 1952-04-29 | Gen Electric | Molded tubular body |
GB784135A (en) * | 1954-03-01 | 1957-10-02 | Hexcel Products Inc | Improvements in or relating to means for forming cellular structures from a pile of webs joined together by spaced glue lines |
DE1777509U (en) * | 1958-08-19 | 1958-11-13 | Friedrich Stelling | PANEL-SHAPED COMPONENT. |
US3114666A (en) * | 1960-05-06 | 1963-12-17 | Hexcel Products Inc | Method of and means for making honeycomb utilizing helical printing roller |
-
1964
- 1964-04-20 US US360955A patent/US3321355A/en not_active Expired - Lifetime
-
1965
- 1965-04-08 JP JP40020369A patent/JPS5146782B1/ja active Pending
- 1965-04-14 DE DE1965H0055786 patent/DE1504368B1/en active Pending
- 1965-04-20 GB GB16658/65A patent/GB1076076A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
JPS5146782B1 (en) | 1976-12-10 |
US3321355A (en) | 1967-05-23 |
DE1504368B1 (en) | 1970-11-12 |
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